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首页> 外文期刊>Journal of Aircraft >Fast Tool for Buckling Analysis and Optimization of Stiffened Panels
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Fast Tool for Buckling Analysis and Optimization of Stiffened Panels

机译:加筋板屈曲分析和优化的快速工具

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摘要

This paper presents a fast tool that can be used during the preliminary design of isotropic and composite stiffened panels subjected to axial compression. It consists of two modules, one for the analysis and one for the optimization. The analysis is performed by implementing an analytical formulation to obtain the linearized buckling load and to study the nonlinear postbuckling field. In particular, closed-form solutions are derived for the linearized local and global buckling loads, and a semi-analytical procedure is implemented for the study of the nonlinear local postbuckling field. The optimization is based on genetic algorithms and allows taking into account buckling and postbuckling requirements with reduced computational time. Two examples regarding the minimum weight optimization of an isotropic panel and a composite panel are discussed and verified by means of finite element eigenvalue and nonlinear analyses. The total time required for the analysis and the optimization is of the order of a few minutes, and the difference between the analytical and numerical results is below 9% for the buckling load and below 3% for the postbuckling stiffness.
机译:本文介绍了一种快速工具,该工具可用于经受轴向压缩的各向同性和复合材料加劲板的初步设计中。它由两个模块组成,一个用于分析,一个用于优化。通过执行分析公式来执行分析,以获得线性屈曲载荷并研究非线性后屈曲场。尤其是,针对线性化的局部和整体屈曲载荷导出了封闭形式的解,并为研究非线性局部后屈曲场实施了半解析程序。该优化基于遗传算法,并允许考虑屈曲和后屈曲需求,并减少了计算时间。通过有限元特征值和非线性分析,讨论并验证了有关各向同性面板和复合面板最小重量优化的两个例子。分析和优化所需的总时间约为几分钟,并且屈曲载荷的分析结果和数值结果之间的差值低于9%,而屈曲后刚度的数值结果则低于3%。

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